DocumentCode
3186253
Title
Simulation and experimental research on thermal protection of the memory embedded missile based on ANSYS
Author
Feng, Wen ; Xiao-ping, Yang ; Zhao-kui, Diao
Author_Institution
Nat. Key Lab. of Electron. Meas., Technol. North Univ. of China, Taiyuan, China
fYear
2010
fDate
3-5 Dec. 2010
Firstpage
236
Lastpage
239
Abstract
The relationship between the object temperature and time during heat transfer was analyzed with the basic principles of heat and mass transfer for the effective thermal protection of the memory. Thermal protection structure was simulated with ANSYS 10.0 and validated by experiment. The result demonstrated that nanometer aerogel which was placed between memory and protective layer, 5mm thick and the thermal conductivity is 0.01 w/ (m.k), makes sure the memory works two hours normally in the environment which the temperature is 125°C. It has some referential value to the protection of the memory and other small equipments embedded missile.
Keywords
heat transfer; mass transfer; missiles; numerical analysis; thermal barrier coatings; thermal conductivity; thermal insulation; ANSYS 10.0; heat transfer; mass transfer; memory embedded missiles; nanometer aerogel; thermal conductivity; thermal protection structure; Heat transfer; Heating; Materials; Rubber; Temperature distribution; Temperature measurement; ANSYS; Simulation; Thermal conductivity; Thermal protection;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer and Information Application (ICCIA), 2010 International Conference on
Conference_Location
Tianjin
Print_ISBN
978-1-4244-8597-0
Type
conf
DOI
10.1109/ICCIA.2010.6141580
Filename
6141580
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